Flow Characteristics and Cavitation Effect of the Submerged Water Jet Discharged from a Central-Body Nozzle ()
1. Introduction
The concept of the central-body nozzle was introduced in 1980s, and this kind of nozzle was used firstly in mining industry [1] . As high-pressure liquid moves around a blunt-ended central body fixed inside the flow passage of the nozzle, low-pressure zone might appear immediately downstream of the blunt end, which might spur the occurrence of cavitation. Erosion of solid surface will be accelerated provided that cavitation bubbles collapse near the target surface [2] . However, detailed mechanisms underlying such kind of cavitation have rarely been reported. Additionally, quantitative examination of cavitation erosion effect necessitates feasible tech- niques. Furthermore, the shear layer generated between high-velocity water emanating from a central-body noz- zle and ambient water also contributes to the onset of cavitation.
For submerged water jet, flow patterns near the nozzle depend on both nozzle outlet shape and jet pressure [3] . Meanwhile, intense momentum transfer arises between the jet flow and ambient water, which leads to the dis- turbance on jet edge and the dissipation of jet kinetic energy. The position of cavitation zone and wake flow characteristics play an important role in the determination of optimal operation parameters such as standoff dis- tance and the angle between sample surface and jet axis [4] . At present, for submerged water jet, measurement of flow parameter distributions is difficult, particularly at high jet pressure [5] . And the visualization of cavita- tion phenomena near the nozzle is also problematic in this context [6] .
Here, with a thin cylinder intruding into the flow passage of a round nozzle, submerged water jet discharged from a central-body nozzle at jet pressure of 15 MPa is investigated. High speed photography is employed to capture instantaneous fluctuations of jet edge near nozzle outlet. Numerical simulationis conducted to verify ca- vitation effect downstream of the central body. An impingement experiment is carried out to assess the erosion capacity of submerged water jet. It is expected to provide an in-depth demonstration of features of the central- body nozzle and cast light upon cavitation phenomenon in submerged water jet.
2. Experimental set-up
As shown in Figure 1, an experimental system was constructed for studying both flow characteristics and ero- sion capability of submerged water jet. Acylinder central-body is fixed with its axis collinear with the symme- trical axis of the flow passage of the nozzle. Figure 2 schematically shows across section of the nozzle. The axial distance, s, is defined as the indent distance of the central body in the flow passage. Three schemes are accom- plished as s is set to 0.0 mm,
0.5 mm
and
1.0 mm
. It is conceivable that both the wake flow downstream of the central body and cavitation phenomenon are affected by such an indent distance.
3. Fluctuation of jet edge near the nozzle
According to statistical results based upon water jets at jet pressures larger than 10 MPa, unsteady characteristics are evident represented by transient variation of flow parameters and the interaction between jet and ambient medium [7] [8] . Thus it is unambiguous for submerged water jet that jet edge fluctuation undergoes large am- bient water resistance and diversified flow phenomena occur.
Three nozzles corresponding to the three values of s were manufactured and jet pressure of 15 MPa was adopted in the visualization experiment. High speed photography allows for a close observation of jet edge [9] . Parallel to some practical applications of water jet, the jet segment within the stream wise distance of 10.0 mm from the nozzle outlet section was focused. The image-recording frequency was set to 5000 fps. An LED light of 100 W was used as the auxiliary light source. Image-taking was performed as water jet became fully devel- oped.
Instantaneous variation of jet edge with sampling time is presented in Figure 3 where the time interval be- tween every two adjacent images is 0.2 ms. At s =
0.0 mm
, cross-section width of the jet stream is large com- pared with the other two conditions. While in Figure 3(b) and Figure 3(c), variations of jet width are analogous. A further demonstration of the similitude and difference of the three schemes is depicted in Figure 4 where the monitored cross-section is
3.0 mm
away from nozzle outlet section.
It is shown in Figure 4 that cross-section width of the jet stream at s =
0.0 mm
remains the largest for all the sampling period. However, the corresponding fluctuation magnitudes are much lower than those associated with the other two schemes. At s =
0.5 mm
and s =
1.0 mm
, fluctuation features are similar, and the fluctuation fre- quencies agree well with each other.
4. Numerical simulation
With existing flow visualization techniques, it is questionable to discern jet stream in obtained images under submerged conditions. Numerical simulation was utilized to depict complex flows downstream of nozzle outlet.
Figure 1. Sketch of the experimentalsystem for submerged water jet.
Figure 2. Cross-sectional view of the central-body nozzle.
(a)(b)(c)
Figure 3. Jet edge fluctuations at different indent distances. (a) s = 0.0 mm; (b) s = 0.5 mm; (c) s = 1.0 mm.
It should be noted that a comparison can be implemented between steady numerical results and statistical expe- rimental results [10] .
4.1. Computational Zone
According to the axially symmetrical assumption of the water jet, one-quarter of the entire computational zone is devoted to simulation. In Figure 5, a cubic computational zone including water jet flow and ambient water is
Figure 4. Variation of jet width on the cross-section
3.0 mm
away from nozzle outlet section.
Figure 5. One-quarter of the entire jet flow zone.
presented. The stream wise length of the computation zone is 40d where d is the outlet diameter of the nozzle outlet section. And the transverse dimensions of the computational zone are 20d × 20d. The total gird number at s =
0.0 mm
is 1,273,705.
4.2. Turbulence model
Based on Reynolds averaged Navier-Stokes (RANS) equations and RNG (Renormalization group) k-e turbulent model, three-dimensional steady and unsteady computations were carried out. Scalable wall function was ap- plied to deal with flows near all solid walls. Velocity-pressure coupling was accomplished automatically with the ANSYS-CFX solver used.
4.3. Cavitation model
The Rayleigh Plesset model was used to model the inception and evolution of cavitation in the computational zone. Relative to other cavitation models, this model is advantageous in terms of modeling cavitation inception and bubble collapse [11] . And the primary and second phases were set to be water and vapor, respectively. The mean nucleation site diameter was set to be 2 × 10−6 m. Cavitation condensation and vaporization coefficients were set to be 0.01 and 50, respectively. Volume fraction of the nucleation sites was set to be 5e−4.
4.4. Boundary conditions
Non-slip boundary condition was set at all solid walls. Uniform pressure distribution was set at the nozzle inlet section. And pressure outlet condition was applied for all outlet sections of the computational zone.
4.5. Results and discussion
4.5.1. Velocity distribution
Dissipation of stream wise velocity along the jet axis is plotted in Figure 6. The maximum velocity occurs at s =
1.0 mm
. At s =
0.0 mm
, the peak velocity is the minimum among the three schemes and the stream wise position corresponding to the velocity peak is approximately
6.0 mm
away from the nozzle outlet section. A velocity valley is seen in each velocity curve, but corresponding stream wise positions are different. Water discharged from the annulus section around the central body concentrates towards a point on the jet axis. And then the wa- ter jet reconstructs itself downstream of such a point. Nevertheless, the position of such a point varies with the indent distance of the central body, which apparently gives rise to different starting points of reorganized water jets.
As shown in Figure 7, three cross sections with axial distances of
1.0 mm
,
3.0 mm
and
5.0 mm
from the noz- zle outlet section are extracted for a demonstration of distributions of velocity and volume fraction of cavitation phase. The three schemes are similar in that a velocity valley is presented near the jet axis. Nevertheless, the most explicit valley is associated with the scheme of s = 0.0 mm. In addition, the maximum velocity magnitude at s = 0.0 mm is the lowest among the three schemes.
4.5.2. Volume fraction of cavitation phase
Two kinds of cavitation mechanisms deserve an elucidation in the submerged water jet considered. One is the shear layer produced by the velocity difference between jet stream and ambient water; the other one is related to the flow patterns adjacent to the downstream end of the central body. Numerical results of cavitation are de- picted in Figure 8 where the three cross sections are identical with those shown in Figure 7. It can be extrapo- lated from Figure 8 that a tongue-shape cavitation zone exists immediately downstream of the central body. In light of the velocity distributions shown in Figure 7, the end of the cavitation zone is in accordance with the po- sition where the water jet reorganizes itself. At s =
0.0 mm
, the end section of the central body is parallel to the nozzle outlet section, thus the cavitation zone covers the longest stream wise distance among the three schemes.
In Figure 8, three-dimensional cavitation zones can be generated through rotating the sectional view around the jet axis by 360˚. Although the maximum volume fraction of cavitation phase appears at the jet axis, the im- pingement effect exerted on the sample surfaceis inseparable from peripheral cavitation bubbles.
To relate the cavitation zone shape with jet pressure, a simulation for the scheme of s = 0.0 mm was per- formed at jet pressure of 20 MPa. And the results are shown in Figure 9. It is observable that axial length of the cavitation zone is increased accordingly and the tongue shape is well kept in this context. Through the compari- son of Figure 8 with Figure 9, it is proved that cavitation effect is determined by dual factors, low-pressure zone after the central body and shear effect between jet stream and ambient water. And the former is compara- tively influential.
5. Impingement experiment
To gain a further insight into submerged water jet discharged from the central-body nozzle, an experiment was conducted with sandstone samples at jet pressure of 15 MPa. The nozzle corresponding to the scheme of s = 0.0 mm was used in the experiment and a round nozzle with equivalent outlet diameter was applied to produce a submerged water jet for comparison. Mass weighting method was used and the mass of removed sandstone ma- terial was measured after the impingement.
For the two water jets subject respectively to the two nozzles, five samples with the same dimensions were tested at the same standoff distance of 3.0 mm and the same impingement period of ten seconds. The results are shown in Figure 10.
As shown in Figure 10, The overall mass of removed sandstone with the central-body nozzle is larger than that with the round nozzle. For the corresponding relation between jet pressure and velocity, the jet discharged from the central-body nozzle bears a large bulk velocity and a thin annulus jet layer, so the impingement capa- bility is favorable relative to the round water jet. As the standoff distance is increased to
5.0 mm
, impingement effect signified by the mass of material removed is shown in Figure 11.
Compared with Figure 10, Figure 11 indicates that the discrepancy among the five cases is remarkable. With
Figure 6. Velocity dissipation along the jet axis.
(a) (b)(c)
Figure 7. Velocity distributions on different transverse sections. (a) s = 0.0 mm; (b) s = 0.5 mm; (c) s = 1.0 mm.
the central-body nozzle, a strong fluid-solid interaction is verified thereby. According to numerical results, the standoff distance of
5.0 mm
corresponds to the front end of the cavitation tongue. Therefore it can be estimated that cavitation effect accelerates the erosion of sandstone material. Although the distance between the nozzle outlet and the target sample surface increases, the impingement effect remains almost unaltered. For the round water jet, energy dissipation with increased standoff distance has a significant influence on impingement effect, as evidenced in Figure 11.
6. Concluding Remarks
For submerged water jet discharged from the central-body nozzle, instantaneous variation of jet width is evident. For the scheme in which the end cross section of the central bodyis parallel to the nozzle outlet section, overall jet width is the largest but the jet width fluctuation is the slightest. Cavitation tongue exists in the wake flow immediately downstream of the central body. Stream wise length of cavitation tone is determined by both axial
(a) (b)(c)
Figure 8. Volume fraction of cavitation phase at 15 MPa. (a) s = 0.0 mm; (b) s = 0.5 mm; (c) s = 1.0 mm.
Figure 9. Volume fraction of cavitation phase at 20 MPa associated with the scheme of s = 0.0 mm.
Figure 10. Mass of removed sandstone at standoff distance of
3.0 mm
.
Figure 11. Mass of removed material at standoff distance of
5.0 mm
.
position of the central body and jet pressure. At the same jet pressure, impingement effect is strong with the central-body nozzle, particularly as the target surface is at the front end of the cavitation zone. The mass of the material removed indicates evidently that cavitation reinforces impingement effect.
Acknowledgements
This study is financially supported by National Natural Science Foundation of China (Grant No. 51205171). The authors of this paper also would like to extend their gratitude to Postdoctoral Science Foundation of Jiangsu Province of China (Grant No. 1201026B).